N937FR
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
17 reports on file, 2005-12-21 – 2011-03-17.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 21,951 hrs · 10,595 cycles
F/O WINDSHIELD CRACKED FOLLOWING ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O WINDSHIELD WITH SERVICEABLE WINSHIELD REF AMM 56-11-11-400-000-001.
Part: HINGE FITTING — CORRODED (LT MLG DOOR) · corrosion level 2 · airframe 21,905 hrs · 10,568 cycles
A/C C-CHECK: NON ROUTINE; FWD AIRFRAME HINGE FITTING FOR LT MAIN GEAR DOOR, FWD LUG FACE OF FITTING, HAS WEAR .013" TO .018" DEEP. CAUSED BY BOLT ROTATING. SPOT FACED FWD LUG BOLT HOLE FACE AND INSTALLED BUSHING. MILLED BUSHING TO LUG THICKNESS. FABRICATED WASHER OF 2024T3 .032 MATERIAL IAW EA A9-53R-32010.
Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,905 hrs · 10,568 cycles
ACFT C-CHECK: NON ROUTINE; MAIN CABIN FLOOR SILL BEAM (L2 DOOR) CORRODED BEYOND LIMITS AT FR 66, Y 1732 IAW SRM 53-41-14, P 4.B, FIG. 101. BLENDED CORROSION TREATED AND PRIMED. INSTALLED REPAIR WITH FILLER AND 2 SPLICE ANGLES. SRM 53-41-14, 2(P) AND (Q).
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,905 hrs · 10,568 cycles
ACFT C-CHECK: NON ROUTINE NR 31644; MAIN CABIN FLOORBEAM HAS CORROSION 6" OF FR 66, Y 1732. CORROSION NOTED IS EXFOLIATION AND OUT OF LIMITS IAW SRM 53-41-14 P 103/104, R & R FLOORBEAM ASSY.
Earlier reports · 2005–2010 · 13 reports
2010
Part: PITCH CONTROL — MALFUNCTIONED · airframe 20,358 hrs · 9,831 cycles
PILOT REPORTED, ACFT PITCH WILL NOT STABLE WHILE HAND FLYING, UNCOMMANDED INCREASE IN PITCH UP. MX PERFORMED BITE TEST OF THE EFCS IAW AMM 27-96-00-740-001 WITH NO DEFECTS NOTED. PERFORMED OPS TEST OF THE AFS IAW AMM 22-96-00-710-001 WITH NO DEFECTS NOTED. PERFORMED OPS TEST OF THE TRIMMABLE HORIZ STAB IAW AMM 27-44-00-710-003 WITH NO DEFECTS NOTED. OK TO CONTINUE SERVICE. NOTE: NO PARTS/SYS FOUND DEFICTIVE. REPORT DEFECTIVE. REPORT SUBMITTED AS PRECAUTION PER ACI.
Part: SERVO — WORN (RT ELEVATOR) · airframe 18,388 hrs · 8,928 cycles
AIR TURN BACK DUE TO AIRFRAME VIBRATION ON CLIMB OUT. AIRSPEED 280 KIAS. ALTITUDE APPROX 17,000 FT. LOW FREQUENCY SIGNIFICANT AMPLITUDE INCREASING WITH FORE AND AFT MOVEMENT OF SIDE STICK. MX R & R LT ELEVATOR GREEN SYS SERVO AND RT ELEVATOR YELLOW SYS SERVO IAW AMM 27-34-51 PB 401. LT ELEVATOR BLUE SYS ROD END IAW AMM 27-34-51-420-061. LT ELEVATOR NR 1, 2, AND 3 HINGE FITTINGS HARDWARE AND RT ELEVATOR NR 2 AND 3 HINGE FITTINGS HARDWARE IAW AMM 27-34-41-420-051. MX PERFORMED ELEVATOR FREE PLAY CHECK IAW AMM 27-34-00-200-001. OPS CHECK FLIGHT COMPLETED SATISFACTORY. PN REPLACED: SERVO PN 31075-440, SN 10022, SERVO PN 31075-440 SN 10018, ROD END PN 341203-500, SN 4132.
Part: CYLINDER — LOW (OXYGEN SYSTEM) · airframe 18,258 hrs · 8,861 cycles
DURING CRUISE ALTITUDE THE FLIGHT CREW NOTED THE CREW OXYGEN LOW. MAINTENANCE SERVICED THE CREW OXYGEN AND RESET THE CREW OXYGEN MASKS IAW AMM 12-35-10 PB301, NO LEAKS NOTED.
2009
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOORBEAM Y1292 AND FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 53-41-14, 51-42-11 AND DRAWING D53472780.
Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE LT SHEAR PLATE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE LT SHEAR PLATE IAW SRM 52-41-11, 52-42-21 AND EA A0-53T-31040.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOOR SUPPORT Y1292 AFT OF FRAME 66 AND FWD OF FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11 AND DWG D53472780.
Part: SILL — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE L2 DOOR SILL PLATE HAS CORROSION AT FRAME 68. MX REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA A9-53R-31275.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE R2 DOOR LONGITUDINAL FLOORBEAM -Y1292 AFT OF FRAME 66 HAS CORROSION AROUND NUTPLATES. MAINT REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31267.
Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE RT SIDE LATERAL SHEAR PLATE WAS CORRODED AT FRAME 69 AND FRAME 70. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11 AND EA A0-53T-31040.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 16,532 hrs · 8,075 cycles
DURING C3 C-CHECK, INSP NOTED THE L2 DOOR LONGITUDINAL FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31266.
2008
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,298 hrs · 5,581 cycles
DURING C2 C CHECK, INSPECTION REPORTED A HOLE WAS PUNCTURED INTO THE UPPER SKIN OF AFT CARGO PIT FLOOR PANEL 151VG, NEAR THE FORWARD EDGE, IN THE CENTER. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14 PB 401. UPON COMPLETION OF THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE.
2007
Part: ENGINE — FAILED (NR 1) · airframe 10,478 hrs · 5,192 cycles
FLIGHT CREW REPORTED INFLIGHT SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY/OIL PRESSURE. NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. 1/7/008 FLT CREW REPORTED NT 1 ENGINE FAILURE IN FLT. SMELLED BURNING OIL, CLASS II ECAM ENGINE NR 1 OIL FILTER CLOG, OIL PRESSURE & QTY NORMAL. WITHIN 5 MINUTES, OIL QTY DROPPED TO BELOW 5 QTS. WITHIN 1 MINUTE, NR 1 ENGINE FAILURE. ENGINE SHUT DOWN AS PER ECAM ACTIONS. DISCHARGED AGENT 1. AFTER LANDING NO FIRE INDICATIONS WERE NOTED. R & R NR 1 ENGINE IAW TASK CARDS MP 71042-1 AND MP 71042-2 AND EA A9-72R-12347. CHECKED GOOD, NO FAULTS OR LEAKS NOTED. PERFORMED CAT 3 TEST IAW AMM 22-97-00-710-001. CAT 3B STATUS RETAINED.
2005
Part: ACTUATOR — TRIPPED (SLATS) · airframe 2,948 hrs · 1,436 cycles
UPON APPROACH, FLIGHT CREW REPORTED ECAM F/CTL SLATS FAULT. PERFORMED TSM TASK 27-81-00-810-810. FOUND TORQUE LIMITERS POPPED ON SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM. REPLACED SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM PER AMM 27-84-49-000-001 AND 27-84-49-400-001. PERFORMED SLATS OPS TEST PER AMM 27-84-00-710-001. OPS TEST GOOD.